SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 VU4

2018 VU4

2018 VU4 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.752 AU and a period of 0.65 yr.

Aten Observations: 35
Orbital Period · P
0.65 yr
v(q)
56.5 km/s
v(Q)
20.9 km/s
Diameter · ≈
0.06 km
TJ
7.54
Eccentricity · e
0.4599

Orbit and dynamics

The path is an ellipse reaching 0.406 AU from the Sun at perihelion and 1.098 AU at aphelion, a radial span of 0.692 AU.

Applying Kepler's third law to a = 0.752 AU gives an orbital period of 0.65 yr, or about 238 days.

The high eccentricity (0.46) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 22.77° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 56.5 km/s at perihelion and falls to 20.9 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 23.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 35 observations and has a weighted RMS residual of 0.4001 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

About these computed values

Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Orbital Parameters

Semi-Major Axis
0.7524 AU
Eccentricity
0.4599
Perihelion
0.406 AU
Aphelion
1.098429 AU
Inclination
22.77°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
75.44°

Orbit diagram

The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.

3D orbit (interactive)

Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.

Close approaches

Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).

Date (UTC)Miss distanceVelocity
2029-Oct-06 20:02 0.337547 AU
50496267 km
19.54 km/s
2031-Oct-14 19:41 0.224569 AU
33595098 km
14.46 km/s
2033-Nov-01 16:37 0.107834 AU
16131787 km
13.29 km/s
2035-Nov-14 17:44 0.050166 AU
7504654 km
14.99 km/s
2037-Nov-13 01:59 0.149066 AU
22299900 km
20.77 km/s
2039-Nov-05 21:52 0.359337 AU
53756064 km
28.15 km/s
2044-Oct-07 07:42 0.322301 AU
48215550 km
21.45 km/s
2046-Oct-11 00:21 0.234318 AU
35053522 km
15.34 km/s
2050-Nov-12 18:16 0.049719 AU
7437850 km
14.18 km/s
2052-Nov-14 02:34 0.064683 AU
9676476 km
19.08 km/s
2054-Nov-07 23:32 0.195481 AU
29243487 km
26.19 km/s
2059-Oct-09 06:57 0.294833 AU
44106415 km
23.43 km/s
2061-Oct-08 06:11 0.248806 AU
37220861 km
16.64 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
23.9

Orbit Quality

RMS
0.40013
Condition
7
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

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